Variation of peak pitching-moment coefficients for six airfoils as affected by compressibility /
Harold E. Cleary.

Description

Main Author

Cleary, Harold E.

Related Names

Langley Aeronautical Laboratory.
United States. National Advisory Committee for Aeronautics.

Language(s)

English

Published

Washington, D.C. : National Advisory Committee for Aeronautics, [1944]

Subjects

Wind tunnel testing.
Propellers, Aerial.
Pitching (Aerodynamics)
Compressibility.
Charts, diagrams, etc.
Aerofoils.
Aerodynamic load.
Charts, diagrams, etc.
Wind tunnel testing.
Compressibility.
Pitching (Aerodynamics)
Aerodynamic load.
Aerofoils.
Propellers, Aerial.

Summary

Pressure-distribution tests of six NACA 16-series propeller sections with 1-foot chords were conducted in the NACA 8-foot high-speed tunnel to determine the compressibility effects on peak section pitching-moment coefficients. The data are presented as curves of peak section pitching-moment coefficient against Mach number , thickness ratio, and camber.

Note

Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia.
Originally issued as NACA as Advance Confidential Report L4H17 (October 1944).
NACA Wartime Report L-515.

Physical Description

12, [14] p. : ill. ; 27 cm.

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